ATE426052T1 - CERAMIC WARM LAYER - Google Patents
CERAMIC WARM LAYERInfo
- Publication number
- ATE426052T1 ATE426052T1 AT06764032T AT06764032T ATE426052T1 AT E426052 T1 ATE426052 T1 AT E426052T1 AT 06764032 T AT06764032 T AT 06764032T AT 06764032 T AT06764032 T AT 06764032T AT E426052 T1 ATE426052 T1 AT E426052T1
- Authority
- AT
- Austria
- Prior art keywords
- thermal barrier
- coating
- component
- barrier coating
- hand
- Prior art date
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
- C23C28/3215—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
- C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/36—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
- Inorganic Insulating Materials (AREA)
- Insulated Conductors (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
A ceramic thermal barrier coating (8) for coating the surface (7) of a component (1) of a nickel-based superalloy, and an adhesive coating optionally applied thereon (6), preferably a gas turbine component, includes zirconium oxide (ZrO2) stabilized by yttrium oxide (Y2O3) and production-related impurities, as well as at least one high-temperature and oxidation resistant intermetallic compound, for example NiAl, YRh, ErIr, the volume fraction of which decreases continuously or in stages as the distance from the surface (7) of the component (1)/the adhesive coating (6) increases. Advantageously, a less steep stress gradient is produced by gradually varying the composition of the thermal barrier coating (8). This leads to an increased expansion tolerance of the thermal barrier coating (8) and thus, on the one hand, to an increased lifetime under thermal loading (no flaking) and, on the other hand, the possibility of applying thicker thermal barrier coatings (8), and there for of using the coated components (1) at higher temperatures.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH11522005 | 2005-07-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE426052T1 true ATE426052T1 (en) | 2009-04-15 |
Family
ID=35985842
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT06764032T ATE426052T1 (en) | 2005-07-12 | 2006-07-04 | CERAMIC WARM LAYER |
Country Status (5)
Country | Link |
---|---|
US (2) | US7666516B2 (en) |
EP (1) | EP1902160B1 (en) |
AT (1) | ATE426052T1 (en) |
DE (1) | DE502006003197D1 (en) |
WO (1) | WO2007006681A1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1902160B1 (en) | 2005-07-12 | 2009-03-18 | Alstom Technology Ltd | Ceramic heat insulating layer |
US7800021B2 (en) * | 2007-06-30 | 2010-09-21 | Husky Injection Molding Systems Ltd. | Spray deposited heater element |
FR2960242B1 (en) | 2010-05-18 | 2015-05-01 | C R M A | PROCESS FOR MANUFACTURING MULTI-LAYER COMPONENTS HAVING INCLINED HOLES AND RESISTANT TO HIGH THERMAL CONSTRAINTS AND USE OF THE PROCESS FOR REPAIRING WORKPIECES |
US20160298467A1 (en) * | 2013-11-18 | 2016-10-13 | United Technologies Corporation | Article having variable coating |
US8939706B1 (en) | 2014-02-25 | 2015-01-27 | Siemens Energy, Inc. | Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface |
US20150275682A1 (en) * | 2014-04-01 | 2015-10-01 | Siemens Energy, Inc. | Sprayed haynes 230 layer to increase spallation life of thermal barrier coating on a gas turbine engine component |
US9869013B2 (en) | 2014-04-25 | 2018-01-16 | Applied Materials, Inc. | Ion assisted deposition top coat of rare-earth oxide |
CN107429570B (en) * | 2015-04-17 | 2020-06-09 | 三菱日立电力系统株式会社 | Steam turbine rotor blade and method for manufacturing steam turbine rotor blade |
CN106435566B (en) * | 2016-09-12 | 2018-09-25 | 广西大学 | A kind of method of niobium alloy surface laser multiple tracks cladding composite ceramics gradient coating |
IT201900003691A1 (en) * | 2019-03-13 | 2020-09-13 | Nuovo Pignone Tecnologie Srl | Abrasive terminal of a rotor blade for a turboexpander |
CN113373408B (en) * | 2021-05-14 | 2022-08-09 | 中国航发北京航空材料研究院 | Dysprosium-doped gadolinium zirconate thermal barrier coating material and preparation method of coating |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3912235A (en) * | 1974-12-19 | 1975-10-14 | United Technologies Corp | Multiblend powder mixing apparatus |
JPS62156938A (en) * | 1985-12-28 | 1987-07-11 | 航空宇宙技術研究所 | Manufacture of leaning-function material |
US5236787A (en) * | 1991-07-29 | 1993-08-17 | Caterpillar Inc. | Thermal barrier coating for metallic components |
WO1993005194A1 (en) * | 1991-09-05 | 1993-03-18 | Technalum Research, Inc. | Method for the production of compositionally graded coatings |
CN1074689C (en) * | 1996-04-04 | 2001-11-14 | E·O·帕通电子焊接研究院电子束工艺国际中心 | Method of producing on substrate of protective coatings with chemical composition and structure gradient across thickness and with top ceramic layer |
US5998003A (en) * | 1998-09-10 | 1999-12-07 | Electric Power Research Institute, Inc. | Multilayer nanostructured ceramic thermal barrier coatings |
US6352788B1 (en) | 2000-02-22 | 2002-03-05 | General Electric Company | Thermal barrier coating |
US6503575B1 (en) * | 2000-05-22 | 2003-01-07 | Praxair S.T. Technology, Inc. | Process for producing graded coated articles |
US6544665B2 (en) | 2001-01-18 | 2003-04-08 | General Electric Company | Thermally-stabilized thermal barrier coating |
US6502304B2 (en) * | 2001-05-15 | 2003-01-07 | General Electric Company | Turbine airfoil process sequencing for optimized tip performance |
EP1451382A1 (en) | 2001-11-09 | 2004-09-01 | Alstom Technology Ltd | Method for developing a nickel-base super alloy |
DE10305912B4 (en) | 2003-02-13 | 2014-01-30 | Alstom Technology Ltd. | Hybrid blade for thermal turbomachinery |
DE10313489A1 (en) | 2003-03-26 | 2004-10-14 | Alstom Technology Ltd | Thermal turbomachine with axial flow |
DE10313490A1 (en) | 2003-03-26 | 2004-10-14 | Alstom Technology Ltd | Thermal turbomachine with axial flow |
EP1815035A2 (en) | 2004-11-18 | 2007-08-08 | Alstom Technology Ltd | Nickel-based superalloy |
JP4636319B2 (en) * | 2005-04-08 | 2011-02-23 | 住友金属工業株式会社 | Ti alloy, Ti alloy member and manufacturing method thereof |
EP1902160B1 (en) | 2005-07-12 | 2009-03-18 | Alstom Technology Ltd | Ceramic heat insulating layer |
-
2006
- 2006-07-04 EP EP06764032A patent/EP1902160B1/en not_active Not-in-force
- 2006-07-04 DE DE502006003197T patent/DE502006003197D1/en active Active
- 2006-07-04 WO PCT/EP2006/063826 patent/WO2007006681A1/en not_active Application Discontinuation
- 2006-07-04 AT AT06764032T patent/ATE426052T1/en not_active IP Right Cessation
-
2008
- 2008-01-04 US US11/969,257 patent/US7666516B2/en not_active Expired - Fee Related
-
2010
- 2010-01-04 US US12/651,624 patent/US20100104764A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US20080241560A1 (en) | 2008-10-02 |
WO2007006681A1 (en) | 2007-01-18 |
EP1902160B1 (en) | 2009-03-18 |
US7666516B2 (en) | 2010-02-23 |
DE502006003197D1 (en) | 2009-04-30 |
US20100104764A1 (en) | 2010-04-29 |
EP1902160A1 (en) | 2008-03-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
REN | Ceased due to non-payment of the annual fee |